NL6811392A - - Google Patents
Info
- Publication number
- NL6811392A NL6811392A NL6811392A NL6811392A NL6811392A NL 6811392 A NL6811392 A NL 6811392A NL 6811392 A NL6811392 A NL 6811392A NL 6811392 A NL6811392 A NL 6811392A NL 6811392 A NL6811392 A NL 6811392A
- Authority
- NL
- Netherlands
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/32—Locking, e.g. by final locking blades or keys
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
- F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
- F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Centrifugal Separators (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH1127568A CH494341A (de) | 1968-07-26 | 1968-07-26 | Rotor für Turbomaschinen |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NL6811392A true NL6811392A (https=) | 1970-01-29 |
Family
ID=4371868
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NL6811392A NL6811392A (https=) | 1968-07-26 | 1968-08-09 |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US3567337A (https=) |
| JP (1) | JPS4924485B1 (https=) |
| BE (1) | BE736540A (https=) |
| CH (1) | CH494341A (https=) |
| DE (1) | DE1751819B1 (https=) |
| FR (1) | FR2013754A1 (https=) |
| GB (1) | GB1274547A (https=) |
| NL (1) | NL6811392A (https=) |
Families Citing this family (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH572155A5 (https=) * | 1974-05-27 | 1976-01-30 | Bbc Sulzer Turbomaschinen | |
| US3954350A (en) * | 1974-06-14 | 1976-05-04 | Motoren-Und Turbinen-Union Munchen Gmbh | Rotor having means for locking rotor blades to rotor disk |
| FR2282038A1 (fr) * | 1974-08-13 | 1976-03-12 | Mtu Muenchen Gmbh | Dispositif pour fixer les aubes mobiles de turbomachines |
| GB2119026B (en) * | 1981-03-25 | 1984-06-20 | Rolls Royce | Aerofoil blade mounting |
| US4500255A (en) * | 1981-04-24 | 1985-02-19 | United States Of America As Represented By The Secretary Of The Air Force | Spacer structure |
| GB2156908A (en) * | 1984-03-30 | 1985-10-16 | Rolls Royce | Bladed rotor assembly for gas turbine engine |
| US4820127A (en) * | 1988-01-29 | 1989-04-11 | Westinghouse Electric Corp. | Blade support and blade assembly |
| US5100292A (en) * | 1990-03-19 | 1992-03-31 | General Electric Company | Gas turbine engine blade |
| US5090198A (en) * | 1990-05-04 | 1992-02-25 | Rolls-Royce Inc. & Rolls-Royce Plc | Mounting assembly |
| EP1130217B1 (de) * | 2000-03-01 | 2005-05-18 | ALSTOM Technology Ltd | Befestigung von Laufschaufeln in einer Turbomaschine |
| DE10120532A1 (de) * | 2001-04-26 | 2002-10-31 | Alstom Switzerland Ltd | Vorrichtung und Verfahren zur Befestigung einer Laufschaufel längs einer innerhalb eines Rotors einer axial durchströmten Turbomaschine verlaufenden Umfangsnut |
| ITMI20012783A1 (it) * | 2001-12-21 | 2003-06-21 | Nuovo Pignone Spa | Sistema di connessione e bloccaggio di pale rotoriche di un compressore assiale |
| US6761538B2 (en) * | 2002-10-31 | 2004-07-13 | General Electric Company | Continual radial loading device for steam turbine reaction type buckets and related method |
| US20050265846A1 (en) * | 2004-06-01 | 2005-12-01 | Przytulski James C | Balance assembly for rotary turbine component and method for installing and/or adjusting balance weight |
| EP1698758B1 (de) * | 2005-02-23 | 2015-11-11 | Alstom Technology Ltd | Axial getrennter Rotor-Schluss |
| FR2897099B1 (fr) * | 2006-02-08 | 2012-08-17 | Snecma | Roue de rotor de turbomachine |
| US8608446B2 (en) * | 2006-06-05 | 2013-12-17 | United Technologies Corporation | Rotor disk and blade arrangement |
| US8267664B2 (en) * | 2008-04-04 | 2012-09-18 | General Electric Company | Axial compressor blade retention |
| DE102010053141B4 (de) * | 2009-12-07 | 2018-10-11 | General Electric Technology Gmbh | Turbinenaggregat mit möglicher Überdrehung des Fußes einer Schaufel bis zum Einbau einer letzten Schaufel |
| JP6118104B2 (ja) * | 2012-12-26 | 2017-04-19 | 川崎重工業株式会社 | プロペラ翼固定機構 |
| US20140199172A1 (en) * | 2013-01-11 | 2014-07-17 | General Electric Company | Turbomachine and method of handling turbomachine components |
| US9896946B2 (en) * | 2013-10-31 | 2018-02-20 | General Electric Company | Gas turbine engine rotor assembly and method of assembling the same |
| DE102013223607A1 (de) * | 2013-11-19 | 2015-05-21 | MTU Aero Engines AG | Rotor einer Strömungsmaschine |
| US10145382B2 (en) | 2015-12-30 | 2018-12-04 | General Electric Company | Method and system for separable blade platform retention clip |
| KR101884712B1 (ko) * | 2016-12-21 | 2018-08-03 | 두산중공업 주식회사 | 로터 블레이드용 로킹 스페이서 |
| KR101920070B1 (ko) * | 2016-12-23 | 2018-11-19 | 두산중공업 주식회사 | 로터 블레이드용 로킹 스페이서 |
| CN115822730B (zh) * | 2022-12-08 | 2024-11-26 | 杭州中能透平机械装备股份有限公司 | 一种汽轮机叶轮结构及其设计安装方法 |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH349624A (de) * | 1957-03-05 | 1960-10-31 | Oerlikon Maschf | Axiale Strömungsmaschine |
| DE1269137B (de) * | 1960-01-07 | 1968-05-30 | Prvni Brnenska Strojirna | Turbomaschinenlaeufer |
| NL123379C (https=) * | 1963-11-01 |
-
1968
- 1968-07-26 CH CH1127568A patent/CH494341A/de not_active IP Right Cessation
- 1968-08-03 DE DE19681751819 patent/DE1751819B1/de active Pending
- 1968-08-09 NL NL6811392A patent/NL6811392A/xx unknown
- 1968-11-27 US US779374A patent/US3567337A/en not_active Expired - Lifetime
-
1969
- 1969-04-24 JP JP44031341A patent/JPS4924485B1/ja active Pending
- 1969-04-28 FR FR6913476A patent/FR2013754A1/fr not_active Withdrawn
- 1969-07-24 GB GB37293/69A patent/GB1274547A/en not_active Expired
- 1969-07-24 BE BE736540D patent/BE736540A/xx unknown
Also Published As
| Publication number | Publication date |
|---|---|
| JPS4924485B1 (https=) | 1974-06-24 |
| US3567337A (en) | 1971-03-02 |
| DE1751819B1 (de) | 1971-01-21 |
| CH494341A (de) | 1970-07-31 |
| GB1274547A (en) | 1972-05-17 |
| BE736540A (https=) | 1970-01-26 |
| FR2013754A1 (https=) | 1970-04-10 |